Drag-free spacecraft as platforms for space missions and fundamental physics

Classical and Quantum Gravity

Volumn 14, Issue 6, 1997, Pages 1549-1555

  DeBra, Daniel B ^a  

^a Stanford University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0031527507     PISSN: 02649381     EISSN: None     Source Type: Journal    
DOI: 10.1088/0264-9381/14/6/026     Document Type: Article

References (30)

1. Bull J S 1973 Precise attitude control of the Stanford relativity satellite Doctoral Dissertation Stanford University
2. Chen J-H 1983 Helium thruster propulsion system for precise attitude control and drag compensation of the Gravity Probe-B satellite Doctoral Dissertation Stanford University
3. Danzmann K 1996 LISA - an ESA cornerstone project for detection and observation of gravitational waves COSPAR, Birmingham, UK FPSI-0010
4. DeBra D B 1970 Drag-free satellite control system technology Conf. on Experiment Tests of Gravitation Theories sponsored by NASA and The European Space Research Organization, held at California Institute of Technology and JPL
5. DeBra D B and Parkinson B W 1988 Engineering technology for physics experiments in space COSPAR Symp. on Relativistic Gravitation Finland
6. DeHoff R L 1975 Minimum thrusters control of a spinning drag-free satellite, including the design of a large cavity optical sensor Doctoral Dissertation Stanford University
7. Eisner A and Yionoulis S M 1982 NOVA-I - the drag-free navigation satellite ION - National Aerospace Meeting
8. Fleming A W and DeBra D B 1971 The stability of gravity stabilized drag-free satellites AIAA J. 9 1971-80
9. Jafry Y R 1992 Aeronomy coexperiments on drag-free satellites with proportional thrusters: GP-B and STEP PhD Dissertation Stanford University
10. Juillerat R 1970 Physical limitations in sensors for a drag-free deep-space probe Proc. Conf. of Experimental Tests of Gravitational Theories CIT and JPL
11. Lange B O 1964 The drag-free satellite AIAA J. 2 1590-606
12. Lee K-N 1992 Wide dynamic range helium thruster design for the relativity gyroscope satellite PhD Dissertation Stanford University
13. Mobley F F et al 1975 Electromagnetic suspension for the TIP II satellite 13th Int. Conf. on Magnetics
14. Moe K, DeBra D, Van Patten R, Moe M, Delka G and Ruggera M 1976 Exospheric density measurements from the drag-free satellite TRIAD J. Geophys. Res. 81 3753-61
15. Nobili A M 1996 Galileo Galilei 3rd National Workshop (Pisa)
16. Powell J D 1972 Mass center estimation in spinning drag-free satellites J. Spacecraft Rockets 9 399-405
17. Powell J D and DeBra D B 1973 Orbital simulation of satellite accelerations for drag-free control and low-level accelerometers Rev. R. A. I. R. O.
18. Ray C and DeBra D B 1971 Orbital coupling for proof mass control in a partially drag free satellite VIIth IFAC Symp. Automatic Control in Space (Rottach-Egern)
19. Ray C, Jenkins R A, Van Patten R and Junkins J L 1982 Attitude and translation control of a low-altitude GRAVSAT AIAA/AAS Astrodynamics Conf.
20. Sanz S and DeBra D B 1975 Attitude translational coupling in a rotating drag-free satellite AAS/AIAA Specialist Conf. (Nassau)
21. Sanz-DeCordova S 1975 Orientation and three-dimensional mass center estimation in a rotating drag-free satellite Doctoral Dissertation Stanford University
22. Space Department of Johns Hopkins University: Applied Physics Lab, and Guidance and Control Lab of Stanford University 1974 A satellite freed of all but gravitational forces TRIAD I J. Spacecraft 11 637-44
23. Tashker M G 1974 Integral control of a spinning drag-free satellite Doctoral Dissertation Stanford University
24. Tashker M G and DeBra D B 1976 Complex symmetric root square locus with an application to a spinning drag-free satellite VIIth IFAC Symp. (Rottach-Egern)
25. Tisson J 1972 Influence des rayonnements spatiaux sur l'accelerometre CACTUS Note Technique ONERA No 200, Office National d'Etudes et de Recherches Aero-spatiales, Paris
26. Turneaure et al 1988 The Gravity Probe-B relativity gyroscope experiment: development of the prototype flight instrument COSPAR Symp. on Relativistic Gravitation Finland
27. Wiktor P, Chen J-H and DeBra D B 1989 Optimal thruster configuration for the GP-B spacecraft XIth IFAC Symp. on Automatic Control (Tsukuba)
28. Wiktor P, Jafry Y and DeBra D B 1992 On orbit thruster calibration with applications to Gravity Probe-B
29. Worden P W and Everitt C W F 1988 Almost exactly zero: the equivalence principle Near Zero (Fairbank)
30. Yansouni P and DeBra D B 1974 Nonlinear Identification in the DISCOS position sensor AIAA Mechanics and Control of Flight Conf. (Anaheim, CA)